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There is this text “india was always growing under the shadow of Russia and US technology , they always copy cut the technology of the west and the east.” as the first line of the article. Please get it removed. —Preceding unsigned comment added by SunLikeStar (talk • contribs) 08:26, 15 April 2010 (UTC)Reply
The opening paragraph of this article says that the first stage uses solid fuel, but the section on the first stage says that it uses hypergolic (liquid) fuel. Which of these is correct? --Apyule 23:57, 12 July 2006 (UTC)Reply
The first stage is sub-divide into two.
1a which uses solid fuel(HTPB) for the main core booster.
2a which uses liquid fuel(N2O4/UDMH) for the 4 strap-ons.
See table on right hand side below the first .jpeg for details. —Preceding unsigned comment added by 146.232.75.208 (talk • contribs)
There's a neutrality tag applied to the "Launches" section, with no comments at all in here. I'm removing it until someone posts a good reason for disputing GSLV's launches. Jimgeorge 18:08, 2 September 2007 (UTC)Reply
This article was automatically assessed because at least one WikiProject had rated the article as start, and the rating on other projects was brought up to start class. BetacommandBot 18:00, 9 November 2007 (UTC)Reply
The reference to ISRO images (or even the detailed information on failure analysis given in ISRO's 2006-07 annual report) does not mention that the the launcher was intentionally destroyed. 59.96.185.88 (talk) 20:16, 17 April 2008 (UTC)Reply
This has been discussed for similar failures. A single component failure which causes the payload to be lost is an outright failure not a partial failure. "Partial Failure" only applies if the payload is still usable. This is regardless of test objectives met during the flight. Therefore D3 would be an outright failure, not a partial failure. --GW… 11:31, 15 April 2010 (UTC)Reply
There are too many images in this article. It is now getting to a point at which there are display issues, and several images which are displayed under non-free licences are redundant, and hence violate the fair use criteria. I think it would be a good idea to cut down on fair use images. --GW… 13:39, 15 April 2010 (UTC)Reply
It seems that as of late some moron has reintroduced evidence that Insat 4CR went AWOL for 5 days. This claim is ofcourse false as the ISRO refuted the claim that the satellite went AWOL. READ THE LINK BELOW before re-inserting false claims.
The tag that exists on the current version of this article is just stupid. If, as I have been informed, it is standard practice, then that is simply stupidity multiplied.
The tags were created on this project to draw quick attention to something that the reader might not know, e.g., the article is in a state of flux due to it being involved in a current event, or the article is overloaded with bias, or the article is not reliably sourced, etc. But this tag, detailing when the rocket was supposed to launch, what kind of rocket it was, what happened to the rocket, who will get fired because the rocket didn't work, etc, is NOT in keeping with the mission of the tags, when they were first created. This tag is basically a new section of the article. Hey, that's an idea, why not actually just write a section and add it to the article? Oh, but that wouldn't satisfy somebody's urge to tinker endlessly with what I thought was a good thing, but now realize maybe should just be phased out together.
Would somebody please justify to me why we need a tag which offers the detail which should just be in the article? Because right now I have to conclude that tags like these are just the product of some geek who has nothing better to do on the weekends than come up with new ways to hang ornaments on the Wiki-tree, instead of writing frigging articles, which is what we are supposed to be doing. 74.178.230.17 (talk) 03:18, 17 April 2010 (UTC)Reply
Hi! Reference # 7 cannot be traced. Page not found message is found instead. Can we remove that link. பரிதிமதி (talk) 20:31, 9 May 2010 (UTC)Reply
Hi, from the specification detail, after the first stage rocket engine is close, the boosters shall continue burning 60 seconds. In this period, the body of first stage became "dead weight"? Ultrahabbit(talk) 1:57, Oct 29, 2012(UTC)
Yes , the boosters and the first stage are jettisoned together after burnout is complete for both reducing unnecessary complexity. - 994u — Preceding unsigned comment added by 994u (talk • contribs) 08:40, 18 January 2014 (UTC)Reply
Inthis interview, ISRO mentions the December 2013 launch of a variant called GSLV T5, which may be used in 2016 to launch the Chandrayaan-2 rover to the Moon. BatteryIncluded (talk) 15:21, 4 November 2013 (UTC)Reply
The image to the right of the table in the "Launch History" section should be moved to another section to facilitate proper readability. Please make the necessary changes.
Should this page atleast make a reference to GSLV Mk III ?. I understand that the vehicle is a different beast than the GSLV Mk.1,2. But we need a link atleast in the See also section linking the two. — Preceding unsigned comment added by 172.11.20.161 (talk) 21:14, 5 January 2014 (UTC)Reply
Should the launch history include the scheduled launches of the GSLV Mk-III as well? Have included here-in. Feel free to remove if you think it doesn't sound okay. Prad2609 (talk) 18:16, 15 January 2014 (UTC)Reply
The GSLV Mk-III added by me in the launch history section was removed by User:Johnxxx9 commenting that I had confused the Mk-III and Mk-II. I would like to clarify that I had not.
The Mk-III has been cited in the article as a variant in the main article. I thought that since this was the case the launch history must reflect the upcoming launches of this variant as well.
The Mk-III, technically, is not a variant of the GSLV Mk-I or Mk-II. These variants are similar and differ in engines used and not in design. The Mk-III is a whole new design and I think this page should not include the Mk-III in the variants section. On balance, people looking for information on the GSLV Mk-III may also land up on this page due to similarity in name. I propose that the Mk-III be linked to in the also see section rather than in the main article space. I am making these changes and if you feel the thinking is incorrect, kindly explain here and feel free to revert.Prad2609 (talk) 10:59, 19 January 2014 (UTC)Reply
ISRO is still calling it the GSLV Mk III so it would be strange not to include something about it here. Someone added a section under "Variants" and I added a sentence under "History." Both have links to the Mk III article. If we decide that the Mk III is in fact a completely different thing, then we should add a "Not to be confused with" hatnote to the top of the article. But I think that would be wrong. Kendall-K1 (talk) 14:15, 19 December 2014 (UTC)Reply
I've reverted a couple recent edits changing the current, objective and neutral, launch history to one based solely on claims made by first-party sources (i.e. ISRO) with a vested interest. In order to portray the GSLV in the best possible light, ISRO inflate its reliability statistics, claiming D1 and F4 as successful in spite of the former leaving its payload in a completely useless orbit and the latter costing its satellite around five years' fuel. Reliable third-party sources consider these launches an outright failure and a partial failure respectively. It is completely inappropriate to change this based only on the views of an organisation with a clear and visible bias. --W. D. Graham 22:01, 20 January 2014 (UTC)Reply
This article Russian route characterizes launches as "successful, sub-optimal and failed". Anir1uph | talk | contrib 01:00, 31 January 2014 (UTC)Reply
The summary gives the specific impulse of the first stage as 166 which is obviously wrong. (Note that the PSLV page gives the Isp of the essentially identical core stage as 269.) 69.72.92.96 (talk) 21:40, 20 February 2014 (UTC) Also the summary gives the burn time as 100 seconds while the text gives 109 (giving 100 for the S125 used for the first launch only). 69.72.92.35 (talk) 07:49, 21 February 2014 (UTC)Reply
History - GSlV-F02 to GSLV-F02; INx-T-4C to INSAT-4C
The next sentence is garbled; I suggest: GSLV-F04, the fifth GSLV flight, launched INSAT-4CR into a...
Third stage - cyrogenic to cryogenic
Launch History - D6 - six metre to six meters; it's to its 69.72.92.139 (talk) 21:42, 6 September 2015 (UTC)Reply
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The text states that INSAT-3DR is the second heaviest satellite orbited by the GSLV Mark II but the mass given, 2211 kg, is the highest (the other two being 2117 kg for GSAT-6 and 1980 kg for GSAT-14). 69.72.92.100 (talk) 07:45, 11 September 2016 (UTC)Reply
There are now two different future launches labelled F09. 69.72.92.19 (talk) 06:30, 12 September 2016 (UTC)Reply
@JFG: Those recent additions to schedule are not from citable source. Ohsin (talk) 04:41, 27 April 2017 (UTC)Reply
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There are plenty of GSLV images available in net. Someone is promoting a petty engineering college named SJCET by placing a photo of GSLV from their college. I do lack an image with my own copy right. I have informed the ISRO public relation cell to make necessary changes. — Preceding unsigned comment added by Tpvipin (talk • contribs) 14:50, 1 February 2018 (UTC)Reply